Airworthiness Directive

AD 2025-17-08 90 FR 41290 Active

Federal Aviation Administration · 14 CFR part 39

Requires repetitively inspecting the stabilizer actuator to confirm that the stabilizer actuator lock ring is present, correctly seated in the groove in the upper housing, and engaged in the clamp nut; taking applicable…

FR document
2025-16190
Amendment
39-23118
Published
2025-08-25
Effective
2025-09-29
Models covered
1

Last live check: 2026-08-19

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AD

2025-17-08

FR doc 2025-16190 · 90 FR 41290

AD 2025-17-08Published 2025-08-25Effective 2025-09-29

Supersedes 2022-23-08

Supersedence is read from the Federal Register text of the newer AD — the FAA publishes no structured field for it — and names only ADs held in our index.

FAA rule - 14 CFR 39

FAA rule. Compliance with an applicable AD is required under 14 CFR 39.7. Check its effective date, applicability, compliance times and current status.

Requires repetitively inspecting the stabilizer actuator to confirm that the stabilizer actuator lock ring is present, correctly seated in the groove in the upper housing, and engaged in the clamp nut; taking applicable corrective actions; applying a witness mark (torque seal); and installing a secondary retention feature as terminating action for the repetitive inspections.

Full official abstract

The FAA is superseding Airworthiness Directive (AD) 2022-23- 08, which applied to all Viking Air Limited (Viking) Model DHC-3 airplanes. AD 2022-23-08 required a visual inspection of the stabilizer actuator to confirm that the stabilizer actuator lock ring is present, correctly seated in the groove in the upper housing, and engaged in the clamp nut, applicable corrective actions, application of a torque seal, and sending the inspection results to the FAA. Since the FAA issued AD 2022-23-08, Transport Canada, which is the aviation authority for Canada, issued mandatory continuing airworthiness information (MCAI) to address the unsafe condition identified as a missing stabilizer actuator lock ring. This AD requires repetitively inspecting the stabilizer actuator to confirm that the stabilizer actuator lock ring is present, correctly seated in the groove in the upper housing, and engaged in the clamp nut; taking applicable corrective actions; applying a witness mark (torque seal); and installing a secondary retention feature as terminating action for the repetitive inspections. This AD also prohibits installing any stabilizer actuator unless it is a serviceable part. The FAA is issuing this AD to address the unsafe condition on these products.

More directives for de Havilland DHC-3 Otter

  1. AD 2023-22-17 Airworthiness Directives; Viking Air Limited (Type Certificate Previousl... Effective 2024-01-19
  2. AD 2023-18-03 Airworthiness Directives; Viking Air Limited (Type Certificated Previous... Effective 2023-10-24
  3. AD 2022-21-51 Airworthiness Directives; Viking Air Limited (Type Certificate Previousl... Effective 2022-12-01
  4. AD 2022-23-08 Airworthiness Directives; Viking Air Limited (Type Certificate Previousl... Effective 2022-11-02
  5. AD 2022-05-11 Airworthiness Directives; Viking Air Limited (Type Certificate Previousl... Effective 2022-04-13

All de Havilland DHC-3 Otter directives

Applies to 1 model in our index